WO2010108603A1 - Thermally decoupled bearing arrangement - Google Patents

Thermally decoupled bearing arrangement Download PDF

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Publication number
WO2010108603A1
WO2010108603A1 PCT/EP2010/001541 EP2010001541W WO2010108603A1 WO 2010108603 A1 WO2010108603 A1 WO 2010108603A1 EP 2010001541 W EP2010001541 W EP 2010001541W WO 2010108603 A1 WO2010108603 A1 WO 2010108603A1
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WO
WIPO (PCT)
Prior art keywords
bearing
shaft
ring
rotating
stationary
Prior art date
Application number
PCT/EP2010/001541
Other languages
German (de)
French (fr)
Inventor
Dieter Pfeil
Hans-Georg Scherer
Gisela Rauh
Original Assignee
Eagleburgmann Germany Gmbh & Co.Kg
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eagleburgmann Germany Gmbh & Co.Kg filed Critical Eagleburgmann Germany Gmbh & Co.Kg
Priority to CN201080012228.2A priority Critical patent/CN102356246B/en
Priority to US13/138,628 priority patent/US20120068565A1/en
Priority to EP10708731A priority patent/EP2411688B1/en
Priority to BRPI1014193A priority patent/BRPI1014193A2/en
Priority to JP2012500117A priority patent/JP5422040B2/en
Priority to CA2753819A priority patent/CA2753819C/en
Priority to MX2011009887A priority patent/MX2011009887A/en
Publication of WO2010108603A1 publication Critical patent/WO2010108603A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/10Sliding-contact bearings for exclusively rotary movement for both radial and axial load
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D13/00Pumping installations or systems
    • F04D13/02Units comprising pumps and their driving means
    • F04D13/021Units comprising pumps and their driving means containing a coupling
    • F04D13/024Units comprising pumps and their driving means containing a coupling a magnetic coupling
    • F04D13/026Details of the bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/04Shafts or bearings, or assemblies thereof
    • F04D29/046Bearings
    • F04D29/0465Ceramic bearing designs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/12Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
    • F16C17/22Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with arrangements compensating for thermal expansion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C23/00Bearings for exclusively rotary movement adjustable for aligning or positioning
    • F16C23/02Sliding-contact bearings
    • F16C23/04Sliding-contact bearings self-adjusting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/043Sliding surface consisting mainly of ceramics, cermets or hard carbon, e.g. diamond like carbon [DLC]
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/34Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3464Mounting of the seal
    • F16J15/3472Means for centering or aligning the contacting faces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/42Pumps with cylinders or pistons

Definitions

  • the invention relates to a bearing arrangement for supporting a shaft, which is produced from components having different thermal expansion coefficients, wherein the bearing assembly comprises a thermal decoupling.
  • Bearing arrangements are known from the prior art in different embodiments.
  • a bearing shell of the sliding bearing it is often desirable for a bearing shell of the sliding bearing to be made of a wear-resistant material, e.g. a ceramic material.
  • a wear-resistant material e.g. a ceramic material.
  • problems may occur due to the many times higher thermal expansion coefficient of steel compared to the ceramic material. This can lead to damage to the bearing assembly.
  • the bearing assembly according to the invention with the features of claim 1 has the advantage that it enables thermal decoupling on the bearing, so that the individual parts of the bearing assembly can be produced from materials having different thermal expansion coefficients. This allows the materials for the individual components to be optimally adapted to the respective requirements. Furthermore, according to the invention, a structure of the bearing arrangement can be very simple and inexpensive. This is inventively achieved in that a band member is shrunk on an outer circumference of a rotating bearing ring, so that between the band member and rotating bearing ring, a shrink connection is present. Thus, the rotating bearing ring with the shrunk-on band element forms a composite element which is inserted with centering fit in a recess of a retaining ring.
  • the composite element can thus be inserted by hand into the recess of the retaining ring and removed.
  • the band member is connected by means of an axial connection with the retaining ring.
  • the composite element is in the radial direction at least partially from Enclosed retaining element, wherein the thermal decoupling between the composite element and retaining element is possible due to the running with centered fit insertion of the composite element in the retaining element.
  • a stationary bearing ring and the rotating bearing ring thereby form an axial sliding bearing.
  • the stationary bearing ring additionally has a radially inwardly directed sliding surface in order to form a radial plain bearing together with a bearing bush which surrounds the shaft.
  • a radial sliding bearing and an axial sliding bearing can be provided on the stationary bearing ring at the same time.
  • the number of components can be reduced and a particularly compact bearing arrangement can be provided by this multi-surface bearing on the stationary bearing ring.
  • the band element is formed symmetrically to an axis arranged perpendicular to a central axis of the shaft. This ensures that a uniform change in dimensions occur when temperature changes occur on the strip element.
  • the band element particularly preferably has a large chamfer on the two radially outwardly directed edge regions.
  • the bearing arrangement is designed as a double bearing arrangement and thus comprises two rotating and two stationary bearing rings.
  • the shaft can be stored at two spaced-apart areas.
  • the rotating bearing rings are arranged on sides of the stationary bearing rings which are directed towards one another in the axial direction.
  • the rotating bearing rings are arranged between the stationary bearing rings in the axial direction.
  • the rotating bearing rings are arranged in the axial direction on opposite sides of the stationary bearing rings.
  • the stationary bearing rings are arranged in the axial direction between the rotating bearing rings.
  • the present invention relates to a magnetic coupling with a bearing assembly according to the invention. Magnetic couplings are particularly preferably used in speed-controlled machines, especially in pumps.
  • FIG. 1 is a schematic sectional view of a bearing assembly according to a first embodiment of the invention
  • Fig. 2 is a schematic sectional view of a connection arrangement of
  • Fig. 3 is a schematic sectional view of a centrifugal pump, which is a
  • Fig. 4 is a schematic sectional view of a bearing assembly according to a second embodiment.
  • the bearing assembly 1 comprises a cylindrical bearing bush 2, in which a shaft 3 is arranged. Between the bearing bush 2 and the shaft 3, an annular gap 4 is provided, so that between the bearing bush 2 and the shaft 3, a radial distance is present.
  • the size of the annular gap 4 is chosen such that a thermal expansion behavior of the shaft 3 is taken into account, since the shaft 3 and the bearing bush 2 are made of different materials.
  • the shaft 3 are made of a steel material and the bearing bush made of a ceramic material (SiC).
  • the bearing assembly 1 of the embodiment shown serves both for axial and radial support of the shaft 3.
  • the bearing assembly is the first further provided as a double bearing to support the shaft 3 at two spaced apart areas.
  • the bearing assembly comprises a pair of Axialgleitlagern 14, 14 'and a pair of radial plain bearings 15, 15'.
  • the Axialgleitlager 14, 14 'each comprise a rotating bearing ring 7, T and a stationary bearing ring 6, 6'.
  • the radial sliding bearings 15, 15 ' are formed in the radial direction of the shaft between the stationary bearing ring 6, 6' and an outer casing 2b of the bearing bush 2.
  • the two stationary bearing rings 6, 6 ' are fastened to a housing part 5 by means of pins 13, 13'.
  • the shaft 3 is connected to the bearing bush 2 at the two opposite ends of the bearing bush 2 via connecting or centering arrangements 21, 21 '.
  • the connecting assemblies 21, 21 ' are used for the concentric positioning of the bearing bush 2 relative to the shaft 3.
  • Each of the connecting assemblies 21, 21' comprises an annular retaining element 8, 8 ', which are connected by means of pins 12 with the shaft 3.
  • the rotating bearing rings 7, T are part of the connection arrangements 21, 21 '.
  • the connecting arrangements 21, 21 'furthermore also include an additional band-ring element 9, 9'.
  • the band ring element 9, 9 ' is formed symmetrically to an axis A, wherein the axis A is perpendicular to a central axis or axis of rotation XX of the shaft 3.
  • the band ring element 9, 9 ' is made of a metallic material and is shrunk onto the rotating bearing rings 7, 7', which are made of a ceramic material, by means of a shrink connection 22, 22 '.
  • Via a fastening pin 10, 10 ' while the band ring element 9, 9' in the axial direction with the annular support member 8, 8 'is connected.
  • the annular retaining element 8 has a recess 8a, which is bounded radially outwards by an annular edge region 8b.
  • the composite element 23, comprising the rotating bearing ring 7 and the band ring element 9 is inserted with centering fit into the recess 8a and connected only via the mounting pin 10 in the axial direction with the annular support member 8.
  • the rotating bearing ring 7 is still on its inner peripheral portion via a connection 27, in particular a centering fit, connected to the bearing bush 2, wherein the bearing bush 2 is preferably clamped in the axial direction between the holding elements 8, 8 '.
  • the bearing bush 2 is centered centrally on the connection assembly 21 on the shaft 3, so that the shaft 3 and the bearing bush 2 can be easily made of materials with different coefficients of thermal expansion.
  • the band ring element 9 furthermore has large chamfers 9a, 9b on its radially outwardly directed edge regions, these chamfers likewise being formed symmetrically with respect to the axis A.
  • a snap ring 11 is also provided on the chamfer 9b of the band ring member 9 for fixing the composite element 23, which is held in a recess in the edge region 8b.
  • a thermal decoupling between the components with different thermal expansion coefficients can be achieved.
  • the rotating bearing ring 7 and the bearing bush 2 are made of a ceramic material.
  • the rotating bearing ring 7 does not respond to temperature changes by tilting, which can lead to the wear occurring in the prior art on the axial sliding surfaces 7a, 6a of the Axialgleitlagers 14, 14 '.
  • Changes in the tension profile in the shrinkage connection 22 between the band ring element 9 and the rotating bearing ring 7 can be compensated for by the composite element 23 inserted with centering fit.
  • the composite element 23 inserted with centering fit.
  • no tilting of the rotating bearing ring 7 occurs at different temperature expansions of the individual components.
  • Fig. 3 shows the use of the bearing assembly 1 according to the invention in a pump.
  • the pump has a magnetic coupling 16 which comprises driving magnets 17 and driven magnets 18. Between the driving magnets 17 and the driven magnets 18, a split pot 19 is provided.
  • the driven magnets 18 are connected to the shaft 3.
  • An impeller is designated by the reference numeral 20.
  • the bearing assembly 1 according to the invention takes on both the axial and the radial bearing of the shaft 3, wherein on the stationary bearing rings 6, 6 'two bearing surfaces, namely a bearing surface in the axial direction and a bearing surface are provided in the radial direction.
  • Fig. 4 shows a bearing assembly 1 according to a second embodiment of the invention, wherein the same or functionally identical parts are denoted by the same reference numerals as in the first embodiment.
  • the bearing assembly 1 of the second embodiment substantially corresponds to the first embodiment, wherein, in contrast to the first embodiment, an arrangement of the static bearing rings 6, 6 'to the rotating bearing rings 7, T is reversed.
  • the rotating bearing rings 7, T are arranged on sides of the stationary bearing rings 6, 6 'facing away from one another in the axial direction.
  • no continuous bushing is provided, but there are two separate bushings 30, 31 are provided.
  • the two bushings 30, 31 are interconnected via an intermediate element 32.
  • first bearing bush 30 is connected to the shaft 3 via a holding element 33
  • second bearing bush 31 is connected to the shaft 3 via a holding element 34.
  • the band elements 9, 9 ' are again shrunk onto the rotating bearing rings 7, T and fixedly connected by means of fastening pins 10, 10' to the intermediate element 32 in the axial direction.
  • the rotating bearing rings 7, T and the two bearing bushes 30, 31 are again made of a ceramic material and the intermediate member 32 and the two holding elements 33, 34 and the shaft 3 are made of a metallic material, so that these components again different thermal expansion coefficients exhibit.
  • the rotating bearing rings 7, T and the band ring elements 9, 9 'via shrink connections each form a composite element 23, which are inserted with centering fit in the intermediate element 32. A compound of the composite element 23 for torque transmission takes place in the axial direction only via the fastening pins 10, 10 '. Otherwise, this embodiment corresponds to the previous embodiments, so that reference can be made to the description given there.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Sliding-Contact Bearings (AREA)
  • Support Of The Bearing (AREA)
  • Mounting Of Bearings Or Others (AREA)

Abstract

The invention relates to a bearing arrangement for supporting a shaft (3), comprising a bushing (2) in which the shaft (3) is received, a circumferential ring gap (4) being present between the bushing (2) and the shaft (3), and the bushing (2) and the shaft (3) being made of materials having different thermal expansion coefficients; a connection arrangement (21) comprising a retaining element (8; 32, 33, 34) connected to the shaft (3) and a rotating bearing ring (7) in order to provide a centered support of the bushing (2) at the outer circumference (2b) thereof relative to the shaft (3); a stationary bearing ring (6, 6') that is disposed radially outside of the bushing (2) and forms an axial sliding bearing (14) with the rotating bearing ring (7, 7'); and is characterized in that the connection arrangement (21) comprises a circumferential band ring element (9, 9'), wherein the band ring element (9, 9') is connected to the rotating bearing ring (7, 7') by means of a shrinkage connection in order to form a composite element (23), wherein the composite element (23) is inserted in a recess (8a; 32a) of the retaining element (8; 32) with a centering snug fit, and the band ring element (9, 9') is connected to the retaining element (8; 32) in the axial direction (X-X) of the shaft (3).

Description

Thermisch entkoppelte Lageranordnung Thermally decoupled bearing arrangement
Beschreibungdescription
Die Erfindung betrifft eine Lageranordnung zur Lagerung einer Welle, welche aus Bauteilen mit unterschiedlichen Wärmeausdehnungskoeffizienten hergestellt ist, wobei die Lageranordnung eine thermische Entkoppelung umfasst.The invention relates to a bearing arrangement for supporting a shaft, which is produced from components having different thermal expansion coefficients, wherein the bearing assembly comprises a thermal decoupling.
Lageranordnungen sind aus dem Stand der Technik in unterschiedlichen Ausgestaltungen bekannt. Insbesondere bei Gleitlagern ist es häufig erwünscht, dass eine Lagerschale des Gleitlagers zur Verringerung des Verschleißes aus einem verschleißfesten Material, z.B. einem keramischen Material, hergestellt ist. Beim Zusammenwirken einer derartigen Lagerschale mit einer Welle, welche z.B. aus einem Stahlmaterial hergestellt ist, können Probleme infolge des um ein Vielfaches höheren Wärmeausdehnungskoeffizienten von Stahl gegenüber dem keramischen Material auftreten. Dies kann zu Beschädigungen an der Lageranordnung führen.Bearing arrangements are known from the prior art in different embodiments. In particular with plain bearings, it is often desirable for a bearing shell of the sliding bearing to be made of a wear-resistant material, e.g. a ceramic material. In the interaction of such a bearing shell with a shaft, which e.g. is made of a steel material, problems may occur due to the many times higher thermal expansion coefficient of steel compared to the ceramic material. This can lead to damage to the bearing assembly.
Aus der EP 0 563 437 A2 ist eine Lageranordnung bekannt, bei der eine keramische Lagerbuchse gegenüber einer Welle an einem Außenumfang der Buchse mittels einer Widerlageranordnung zentrierend abgestützt ist. Diese Lageranordnung hat sich grundsätzlich bewährt und wird beispielsweise bei Kreiselpumpen verwendet. In jüngster Zeit werden jedoch erhöhte Anforderungen an die Tragfähigkeit gefordert und insbesondere die Wellendurchmesser aufgrund von starker Nachfrage nach größeren Anlagen vergrößert. Weiter kommt es zu einem vermehrten Einsatz von drehzahlgeregelten Maschinen, so dass sich durch Drehzahlregelung verschiedene Betriebspunkte mit unterschiedlicher Wärmeerzeugung ergeben. Hierdurch ist es nicht möglich, die Lageranordnung auf nur genau einen Betriebspunkt auszulegen.From EP 0 563 437 A2 a bearing arrangement is known, in which a ceramic bearing bush is centered relative to a shaft on an outer circumference of the bushing by means of an abutment arrangement. This bearing arrangement has basically proven and used for example in centrifugal pumps. Recently, however, increased load capacity requirements have been demanded and, in particular, shaft diameters have increased due to strong demand for larger equipment. Furthermore, there is an increased use of speed-controlled machines, so that there are different operating points with different heat generation through speed control. As a result, it is not possible to design the bearing assembly to only one operating point.
Es ist daher Aufgabe der vorliegenden Erfindung, eine Lageranordnung bereitzustellen, welche bei einfachem Aufbau und einfacher, kostengünstiger Herstellbarkeit einen sicheren Betrieb auch bei ständigen Drehzahländerungen einer Welle sicherzustellen.It is therefore an object of the present invention to provide a bearing assembly which ensures a simple construction and simple, cost-effective manufacturability safe operation even with constant speed changes of a wave.
Diese Aufgabe wird durch eine Lageranordnung mit den Merkmalen des Anspruchs 1 gelöst. Die Unteransprüche haben vorteilhafte Weiterbildungen der Erfindung zum Gegenstand.This object is achieved by a bearing arrangement with the features of claim 1. The dependent claims have advantageous developments of the invention the subject.
Die erfindungsgemäße Lageranordnung mit den Merkmalen des Anspruchs 1 weist den Vorteil auf, dass sie eine thermische Entkopplung am Lager ermöglicht, so dass die Einzelteile der Lageranordnung aus Materialien mit verschiedenen Wärmeausdehnungskoeffizienten herstellbar sind. Dadurch können die Materialien für die einzelnen Bauteile optimal an die jeweiligen Anforderungen angepasst werden. Erfindungsgemäß kann ferner ein Aufbau der Lageranordnung sehr einfach und kostengünstig sein. Dies wird erfindungsgemäß dadurch erreicht, dass ein Bandelement auf einem äußeren Umfang eines rotierenden Lagerrings aufgeschrumpft ist, so dass zwischen dem Bandelement und rotierendem Lagerring eine Schrumpfverbindung vorhanden ist. Somit bildet der rotierende Lagerring mit dem aufgeschrumpften Bandelement ein Verbundelement, welches mit zentrierendem Passsitz in eine Ausnehmung eines Halterings eingefügt ist. Erfindungsgemäß wird unter einem zentrierenden Passsitz eine Passung verstanden, welche kein Spiel oder ein geringfügiges Spiel im μm-Bereich aufweist. Es darf somit keine Presspassung vorliegen. Das Verbundelement kann somit von Hand in die Ausnehmung des Halterings eingelegt und entnommen werden. Das Bandelement ist mittels einer Axialverbindung mit dem Haltering verbunden. Das Verbundelement wird dabei in radialer Richtung zumindest teilweise vom Halteelement umschlossen, wobei aufgrund der mit zentrierendem Passsitz ausgeführten Einfügung des Verbundelements in das Halteelement die thermische Entkopplung zwischen Verbundelement und Halteelement möglich ist. Ein stationärer Lagerring und der rotierende Lagerring bilden dabei ein Axialgleitlager. Somit können erfindungsgemäß unerwünschte Veränderungen der Laufflächenpositionen am Axialgleitlager aufgrund von thermischen Änderungen kompensiert werden. Hierdurch kann eine Schädigung der Laufflächen durch sogenannten Kantenläufer verhindert werden.The bearing assembly according to the invention with the features of claim 1 has the advantage that it enables thermal decoupling on the bearing, so that the individual parts of the bearing assembly can be produced from materials having different thermal expansion coefficients. This allows the materials for the individual components to be optimally adapted to the respective requirements. Furthermore, according to the invention, a structure of the bearing arrangement can be very simple and inexpensive. This is inventively achieved in that a band member is shrunk on an outer circumference of a rotating bearing ring, so that between the band member and rotating bearing ring, a shrink connection is present. Thus, the rotating bearing ring with the shrunk-on band element forms a composite element which is inserted with centering fit in a recess of a retaining ring. According to the invention is understood by a centering fit a fit, which has no play or a slight play in the micron range. There must therefore be no interference fit. The composite element can thus be inserted by hand into the recess of the retaining ring and removed. The band member is connected by means of an axial connection with the retaining ring. The composite element is in the radial direction at least partially from Enclosed retaining element, wherein the thermal decoupling between the composite element and retaining element is possible due to the running with centered fit insertion of the composite element in the retaining element. A stationary bearing ring and the rotating bearing ring thereby form an axial sliding bearing. Thus, unwanted changes in the tread positions on the axial sliding bearing due to thermal changes can be compensated according to the invention. As a result, damage to the running surfaces can be prevented by so-called edge runners.
Besonders bevorzugt weist der stationäre Lagerring zusätzlich noch eine radial nach innen gerichtete Gleitfläche auf, um zusammen mit einer Lagerbuchse, welche die Welle umgibt, ein Radialgleitlager zu bilden. Hierdurch kann gleichzeitig ein Radialgleitlager und ein Axialgleitlager am stationären Lagerring vorgesehen werden. Durch diese Mehrflächenlagerung am stationären Lagerring kann insbesondere die Bauteileanzahl reduziert und eine besonders kompakte Lageranordnung bereitgestellt werden.Particularly preferably, the stationary bearing ring additionally has a radially inwardly directed sliding surface in order to form a radial plain bearing together with a bearing bush which surrounds the shaft. As a result, a radial sliding bearing and an axial sliding bearing can be provided on the stationary bearing ring at the same time. In particular, the number of components can be reduced and a particularly compact bearing arrangement can be provided by this multi-surface bearing on the stationary bearing ring.
Besonders bevorzugt ist das Bandelement symmetrisch zu einer senkrecht zu einer Mittelachse der Welle angeordneten Achse ausgebildet. Hierdurch wird sichergestellt, dass eine gleichmäßige Änderung von Maßen bei auftretenden Temperaturänderungen am Bandelement auftreten. Das Bandelement weist dabei besonders bevorzugt eine große Fase an den beiden radial nach außen gerichteten Kantenbereichen auf.Particularly preferably, the band element is formed symmetrically to an axis arranged perpendicular to a central axis of the shaft. This ensures that a uniform change in dimensions occur when temperature changes occur on the strip element. The band element particularly preferably has a large chamfer on the two radially outwardly directed edge regions.
Besonders bevorzugt ist die Lageranordnung als Doppellageranordnung ausgebildet und umfasst somit zwei rotierende und zwei stationäre Lagerringe. Hierdurch kann die Welle an zwei voneinander beabstandeten Bereichen gelagert werden. Vorzugsweise sind die rotierenden Lagerringe dabei an in Axialrichtung zueinander gerichteten Seiten der stationären Lagerringe angeordnet. Mit anderen Worten, sind in Axialrichtung die rotierenden Lagerringe zwischen den stationären Lagerringen angeordnet. Alternativ sind die rotierenden Lagerringe in Axialrichtung an voneinander abgewandten Seiten der stationären Lagerringe angeordnet. Mit anderen Worten sind die stationären Lagerringe in Axialrichtung zwischen den rotierenden Lagerringen angeordnet. Ferner betrifft die vorliegende Erfindung eine Magnetkupplung mit einer erfindungsgemäßen Lageranordnung. Magnetkupplungen werden dabei besonders bevorzugt in drehzahlgeregelten Maschinen, insbesondere in Pumpen, verwendet.Particularly preferably, the bearing arrangement is designed as a double bearing arrangement and thus comprises two rotating and two stationary bearing rings. As a result, the shaft can be stored at two spaced-apart areas. Preferably, the rotating bearing rings are arranged on sides of the stationary bearing rings which are directed towards one another in the axial direction. In other words, the rotating bearing rings are arranged between the stationary bearing rings in the axial direction. Alternatively, the rotating bearing rings are arranged in the axial direction on opposite sides of the stationary bearing rings. In other words, the stationary bearing rings are arranged in the axial direction between the rotating bearing rings. Furthermore, the present invention relates to a magnetic coupling with a bearing assembly according to the invention. Magnetic couplings are particularly preferably used in speed-controlled machines, especially in pumps.
Nachfolgend wird die vorliegende Erfindung anhand von bevorzugten Ausführungsbeispielen in Verbindung mit der begleitenden Zeichnung im Detail beschrieben. In der Zeichnung ist:Hereinafter, the present invention will be described in detail by way of preferred embodiments in conjunction with the accompanying drawings. In the drawing is:
Fig. 1 eine schematische Schnittansicht einer Lageranordnung gemäß einem ersten Ausführungsbeispiel der Erfindung,1 is a schematic sectional view of a bearing assembly according to a first embodiment of the invention,
Fig. 2 eine schematische Schnittansicht einer Verbindungsanordnung vonFig. 2 is a schematic sectional view of a connection arrangement of
Fig. 1 ,Fig. 1,
Fig. 3 eine schematische Schnittansicht einer Kreiselpumpe, welche eineFig. 3 is a schematic sectional view of a centrifugal pump, which is a
Lageranordnung nach Fig. 1 verwendet, undBearing arrangement used in FIG. 1, and
Fig. 4 eine schematische Schnittansicht einer Lageranordnung gemäß einem zweiten Ausführungsbeispiel.Fig. 4 is a schematic sectional view of a bearing assembly according to a second embodiment.
Nachfolgend wird unter Bezugnahme auf die Fig. 1 bis 3 eine Lageranordnung 1 gemäß einem ersten Ausführungsbeispiel der Erfindung im Detail beschrieben. Wie aus Fig. 1 ersichtlich ist, umfasst die Lageranordnung 1 eine zylinderförmige Lagerbuchse 2, in welcher eine Welle 3 angeordnet ist. Zwischen der Lagerbuchse 2 und der Welle 3 ist ein Ringspalt 4 vorgesehen, so dass zwischen der Lagerbuchse 2 und der Welle 3 ein radialer Abstand vorhanden ist. Die Größe des Ringspalts 4 wird dabei derart gewählt, dass ein Wärmedehnungsverhalten der Welle 3 berücksichtigt ist, da die Welle 3 und die Lagerbuchse 2 aus verschiedenen Materialien hergestellt sind. Im vorliegenden Ausführungsbeispiel sind die Welle 3 aus einem Stahlmaterial und die Lagerbuchse aus einem keramischen Material (SiC) hergestellt.Hereinafter, a bearing assembly 1 according to a first embodiment of the invention will be described in detail with reference to FIGS. As can be seen from Fig. 1, the bearing assembly 1 comprises a cylindrical bearing bush 2, in which a shaft 3 is arranged. Between the bearing bush 2 and the shaft 3, an annular gap 4 is provided, so that between the bearing bush 2 and the shaft 3, a radial distance is present. The size of the annular gap 4 is chosen such that a thermal expansion behavior of the shaft 3 is taken into account, since the shaft 3 and the bearing bush 2 are made of different materials. In the present embodiment, the shaft 3 are made of a steel material and the bearing bush made of a ceramic material (SiC).
Die Lageranordnung 1 des gezeigten Ausführungsbeispiels dient gleichzeitig zur axialen wie auch radialen Lagerung der Welle 3. Hierbei ist die Lageranordnung 1 ferner als Doppellager vorgesehen, um die Welle 3 an zwei voneinander beabstandeten Bereichen zu lagern. Hierzu weist die Lageranordnung ein Paar von Axialgleitlagern 14, 14' und ein Paar von Radialgleitlagern 15, 15' auf. Die Axialgleitlager 14, 14' umfassen jeweils einen rotierenden Lagerring 7, T sowie einen stationären Lagerring 6, 6'. Die Radialgleitlager 15, 15' sind in Radialrichtung der Welle zwischen dem stationären Lagerring 6, 6' und einem Außenmantel 2b der Lagerbuchse 2 gebildet. Wie aus Fig. 1 ersichtlich ist, sind die beiden stationären Lagerringe 6, 6' an einem Gehäuseteil 5 mittels Stiften 13, 13' befestigt.The bearing assembly 1 of the embodiment shown serves both for axial and radial support of the shaft 3. Here, the bearing assembly is the first further provided as a double bearing to support the shaft 3 at two spaced apart areas. For this purpose, the bearing assembly comprises a pair of Axialgleitlagern 14, 14 'and a pair of radial plain bearings 15, 15'. The Axialgleitlager 14, 14 'each comprise a rotating bearing ring 7, T and a stationary bearing ring 6, 6'. The radial sliding bearings 15, 15 'are formed in the radial direction of the shaft between the stationary bearing ring 6, 6' and an outer casing 2b of the bearing bush 2. As can be seen from FIG. 1, the two stationary bearing rings 6, 6 'are fastened to a housing part 5 by means of pins 13, 13'.
Die Welle 3 ist mit der Lagerbuchse 2 an den beiden einander entgegengesetzten Enden der Lagerbuchse 2 über Verbindungs- bzw. Zentrieranordnungen 21 , 21' verbunden. Die Verbindungsanordnungen 21 , 21' dienen zur konzentrischen Positionierung der Lagerbuchse 2 relativ zur Welle 3. Jede der Verbindungsanordnungen 21 , 21' umfasst ein ringförmiges Halteelement 8, 8', welche mittels Stiften 12 mit der Welle 3 verbunden sind. Ferner sind auch die rotierenden Lagerringe 7, T Teil der Verbindungsanordnungen 21 , 21'. Wie insbesondere aus Fig. 2 ersichtlich ist, umfassen die Verbindungsanordnungen 21 , 21' ferner auch ein zusätzliches Bandringelement 9, 9'. Das Bandringelement 9, 9' ist dabei symmetrisch zu einer Achse A gebildet, wobei die Achse A senkrecht zu einer Mittelachse bzw. Rotationsachse X-X der Welle 3 ist. Das Bandringelement 9, 9' ist aus einem metallischen Material und ist jeweils auf die rotierenden Lagerringe 7, 7', welche aus einem keramischen Material hergestellt sind, mittels einer Schrumpfverbindung 22, 22' aufgeschrumpft. Somit bilden die rotierenden Lagerringe 7, T und die Bandringelemente 9, 9' jeweils ein Verbundelement 23 (Fig. 2). Über einen Befestigungsstift 10, 10' ist dabei das Bandringelement 9, 9' in Axialrichtung mit dem ringförmigen Halteelement 8, 8' verbunden. Wie aus Fig. 2 ersichtlich ist, weist das ringförmige Halteelement 8 eine Ausnehmung 8a auf, welche durch einen ringförmigen Randbereich 8b radial nach außen begrenzt wird. Hierbei ist das Verbundelement 23, umfassend den rotierenden Lagerring 7 und das Bandringelement 9 mit zentrierendem Passsitz in die Ausnehmung 8a eingelegt und lediglich über den Befestigungsstift 10 in axialer Richtung mit dem ringförmigen Halteelement 8 verbunden. Somit wird die Rotation der Welle 3 über das ringförmige Halteelement 8, den Befestigungsstift 10 und das Bandringelement 9 auf den rotierenden Lagerring 7 übertragen. Der rotierende Lagerring 7 ist weiterhin an seinem inneren Umfangsbereich über eine Verbindung 27, insbesondere einen zentrierenden Passsitz, mit der Lagerbuchse 2 verbunden, wobei die Lagerbuchse 2 vorzugsweise in Axialrichtung zwischen den Halteelementen 8, 8' eingespannt ist. Somit ist die Lagerbuchse 2 zentrisch über die Verbindungsanordnung 21 an der Welle 3 zentriert, so dass die Welle 3 und die Lagerbuchse 2 problemlos aus Materialien mit verschiedenen Wärmeausdehnungskoeffizienten hergestellt werden können.The shaft 3 is connected to the bearing bush 2 at the two opposite ends of the bearing bush 2 via connecting or centering arrangements 21, 21 '. The connecting assemblies 21, 21 'are used for the concentric positioning of the bearing bush 2 relative to the shaft 3. Each of the connecting assemblies 21, 21' comprises an annular retaining element 8, 8 ', which are connected by means of pins 12 with the shaft 3. Furthermore, the rotating bearing rings 7, T are part of the connection arrangements 21, 21 '. As can be seen in particular from FIG. 2, the connecting arrangements 21, 21 'furthermore also include an additional band-ring element 9, 9'. The band ring element 9, 9 'is formed symmetrically to an axis A, wherein the axis A is perpendicular to a central axis or axis of rotation XX of the shaft 3. The band ring element 9, 9 'is made of a metallic material and is shrunk onto the rotating bearing rings 7, 7', which are made of a ceramic material, by means of a shrink connection 22, 22 '. Thus, the rotating bearing rings 7, T and the band ring elements 9, 9 'each form a composite element 23 (FIG. 2). Via a fastening pin 10, 10 'while the band ring element 9, 9' in the axial direction with the annular support member 8, 8 'is connected. As can be seen from FIG. 2, the annular retaining element 8 has a recess 8a, which is bounded radially outwards by an annular edge region 8b. Here, the composite element 23, comprising the rotating bearing ring 7 and the band ring element 9 is inserted with centering fit into the recess 8a and connected only via the mounting pin 10 in the axial direction with the annular support member 8. Thus, the rotation of the shaft 3 via the annular support member 8, the fixing pin 10 and the band ring member 9 is transmitted to the rotating bearing ring 7. The rotating bearing ring 7 is still on its inner peripheral portion via a connection 27, in particular a centering fit, connected to the bearing bush 2, wherein the bearing bush 2 is preferably clamped in the axial direction between the holding elements 8, 8 '. Thus, the bearing bush 2 is centered centrally on the connection assembly 21 on the shaft 3, so that the shaft 3 and the bearing bush 2 can be easily made of materials with different coefficients of thermal expansion.
Das Bandringelement 9 weist ferner an seinen radial nach außen gerichteten Kantenbereichen große Fasen 9a, 9b auf, wobei diese ebenfalls symmetrisch zur Achse A gebildet sind. Dabei ist ferner zur Fixierung des Verbundelements 23 ein Sprengring 11 an der Fase 9b des Bandringelements 9 vorgesehen, der in einer Ausnehmung im Randbereich 8b gehalten ist.The band ring element 9 furthermore has large chamfers 9a, 9b on its radially outwardly directed edge regions, these chamfers likewise being formed symmetrically with respect to the axis A. In this case, a snap ring 11 is also provided on the chamfer 9b of the band ring member 9 for fixing the composite element 23, which is held in a recess in the edge region 8b.
Somit kann erfindungsgemäß eine thermische Entkoppelung zwischen den Bauteilen mit unterschiedlichen Wärmeausdehnungskoeffizienten erreicht werden. Hierbei ist neben der Welle 3 auch das ringförmige Halteelement 8 sowie das Bandringelement 9 aus einem metallischen Material hergestellt. Dagegen sind der rotierende Lagerring 7 und die Lagerbuchse 2 aus einem keramischen Material hergestellt. Somit reagiert der rotierende Lagerring 7 bei Temperaturänderungen nicht durch ein Verkippen, was zu den im Stand der Technik auftretenden Verschleißerscheinungen an den axialen Gleitflächen 7a, 6a des Axialgleitlagers 14, 14' führen kann. Änderungen des Spannungsprofils in der Schrumpfverbindung 22 zwischen dem Bandringelement 9 und dem rotierenden Lagerring 7 können durch das mit zentrierendem Passsitz eingelegte Verbundelement 23 ausgeglichen werden. Insbesondere durch die symmetrische Ausgestaltung des Bandringelements 9 zur Achse A tritt bei unterschiedlichen Temperaturausdehnungen der einzelnen Bauteile keine Verkippung des rotierenden Lagerrings 7 auf.Thus, according to the invention, a thermal decoupling between the components with different thermal expansion coefficients can be achieved. Here, in addition to the shaft 3 and the annular support member 8 and the band ring element 9 is made of a metallic material. In contrast, the rotating bearing ring 7 and the bearing bush 2 are made of a ceramic material. Thus, the rotating bearing ring 7 does not respond to temperature changes by tilting, which can lead to the wear occurring in the prior art on the axial sliding surfaces 7a, 6a of the Axialgleitlagers 14, 14 '. Changes in the tension profile in the shrinkage connection 22 between the band ring element 9 and the rotating bearing ring 7 can be compensated for by the composite element 23 inserted with centering fit. In particular, due to the symmetrical design of the band ring element 9 to the axis A, no tilting of the rotating bearing ring 7 occurs at different temperature expansions of the individual components.
Fig. 3 zeigt die Verwendung der erfindungsgemäßen Lageranordnung 1 in einer Pumpe. Die Pumpe weist eine Magnetkupplung 16 auf, welche antreibende Magnete 17 und angetriebene Magnete 18 umfasst. Zwischen den antreibenden Magneten 17 und den angetriebenen Magneten 18 ist ein Spalttopf 19 vorgesehen. Die angetriebenen Magnete 18 sind dabei mit der Welle 3 verbunden. Ein Pumpenrad ist mit dem Bezugszeichen 20 gekennzeichnet. Die erfindungsgemäße Lageranordnung 1 übernimmt dabei sowohl die axiale als auch die radiale Lagerung der Welle 3, wobei an den stationären Lagerringen 6, 6' zwei Lagerflächen, nämlich eine Lagerfläche in Axialrichtung und eine Lagerfläche in Radialrichtung vorgesehen sind.Fig. 3 shows the use of the bearing assembly 1 according to the invention in a pump. The pump has a magnetic coupling 16 which comprises driving magnets 17 and driven magnets 18. Between the driving magnets 17 and the driven magnets 18, a split pot 19 is provided. The driven magnets 18 are connected to the shaft 3. An impeller is designated by the reference numeral 20. The bearing assembly 1 according to the invention takes on both the axial and the radial bearing of the shaft 3, wherein on the stationary bearing rings 6, 6 'two bearing surfaces, namely a bearing surface in the axial direction and a bearing surface are provided in the radial direction.
Fig. 4 zeigt eine Lageranordnung 1 gemäß einem zweiten Ausführungsbeispiel der Erfindung, wobei gleiche bzw. funktional gleiche Teile mit den gleichen Bezugszeichen wie im ersten Ausführungsbeispiel bezeichnet sind. Die Lageranordnung 1 des zweiten Ausführungsbeispiels entspricht im Wesentlichen dem ersten Ausführungsbeispiel, wobei im Unterschied zum ersten Ausführungsbeispiel eine Anordnung der statischen Lageringe 6, 6' zu den rotierenden Lagerringen 7, T umgekehrt ist. Beim zweiten Ausführungsbeispiel sind die rotierenden Lagerringe 7, T an einander in Axialrichtung abgewandten Seiten der stationären Lagerringe 6, 6' angeordnet. Ferner ist beim zweiten Ausführungsbeispiel keine durchgehende Lagerbuchse mehr vorgesehen, sondern es sind zwei separate Lagerbuchsen 30, 31 vorgesehen. Die beiden Lagerbuchsen 30, 31 sind über ein Zwischenelement 32 miteinander verbunden. Weiterhin ist die erste Lagerbuchse 30 über ein Halteelement 33 mit der Welle 3 verbunden und die zweite Lagerbuchse 31 ist über ein Halteelement 34 mit der Welle 3 verbunden. Die Bandelemente 9, 9' sind wieder auf die rotierenden Lagerringe 7, T aufgeschrumpft und mittels Befestigungsstiften 10, 10' fest mit dem Zwischenelement 32 in Axialrichtung verbunden. Hierbei sind die rotierenden Lagerringe 7, T sowie die beiden Lagerbuchsen 30, 31 wieder aus einem keramischen Material hergestellt und das Zwischenelement 32 und die beiden Halteelemente 33, 34 sowie die Welle 3 sind aus einem metallischen Material hergestellt, so dass diese Bauteile wieder unterschiedliche Wärmeausdehnungskoeffizienten aufweisen. Auch bei dieser Ausgestaltung bilden die rotierenden Lagerringe 7, T und die Bandringelemente 9, 9' über Schrumpfverbindungen jeweils ein Verbundelement 23, welche mit zentrierendem Passsitz in das Zwischenelement 32 eingelegt sind. Eine Verbindung des Verbundelements 23 zur Drehmomentübertragung erfolgt in axialer Richtung lediglich über die Befestigungsstifte 10, 10'. Ansonsten entspricht dieses Ausführungsbeispiel den vorhergehenden Ausführungsbeispielen, so dass auf die dort gegebene Beschreibung verwiesen werden kann. Fig. 4 shows a bearing assembly 1 according to a second embodiment of the invention, wherein the same or functionally identical parts are denoted by the same reference numerals as in the first embodiment. The bearing assembly 1 of the second embodiment substantially corresponds to the first embodiment, wherein, in contrast to the first embodiment, an arrangement of the static bearing rings 6, 6 'to the rotating bearing rings 7, T is reversed. In the second embodiment, the rotating bearing rings 7, T are arranged on sides of the stationary bearing rings 6, 6 'facing away from one another in the axial direction. Further, in the second embodiment, no continuous bushing is provided, but there are two separate bushings 30, 31 are provided. The two bushings 30, 31 are interconnected via an intermediate element 32. Furthermore, the first bearing bush 30 is connected to the shaft 3 via a holding element 33, and the second bearing bush 31 is connected to the shaft 3 via a holding element 34. The band elements 9, 9 'are again shrunk onto the rotating bearing rings 7, T and fixedly connected by means of fastening pins 10, 10' to the intermediate element 32 in the axial direction. Here, the rotating bearing rings 7, T and the two bearing bushes 30, 31 are again made of a ceramic material and the intermediate member 32 and the two holding elements 33, 34 and the shaft 3 are made of a metallic material, so that these components again different thermal expansion coefficients exhibit. Also in this embodiment, the rotating bearing rings 7, T and the band ring elements 9, 9 'via shrink connections each form a composite element 23, which are inserted with centering fit in the intermediate element 32. A compound of the composite element 23 for torque transmission takes place in the axial direction only via the fastening pins 10, 10 '. Otherwise, this embodiment corresponds to the previous embodiments, so that reference can be made to the description given there.

Claims

Ansprüche claims
1. Lageranordnung zur Lagerung einer Welle (3), umfassend eine Lagerbuchse (2), in welcher die Welle (3) aufgenommen ist, wobei zwischen der Lagerbuchse (2) und der Welle (3) ein umlaufender Ringspalt (4) vorhanden ist, und wobei die Lagerbuchse (2) und die Welle (3) aus Materialien mit unterschiedlichen Wärmeausdehnungskoeffizienten hergestellt sind, eine Verbindungsanordnung (21), welche ein mit der Welle (3) verbundenes Halteelement (8; 32, 33, 34) und einen rotierenden Lagerring (7) umfasst, um eine zentrierende Abstützung der Lagerbuchse (2) an ihrem Außenumfang (2b) gegenüber der Welle (3) bereitzustellen, einen stationären Lagerring (6, 6') der radial außerhalb der Lagerbuchse (2) angeordnet ist, und mit dem rotierenden Lagerring (7, 71) ein Axialgleitlager (14) bildet, dadurch gekennzeichnet, dass die Verbindungsanordnung (21) ein umlaufendes Bandringelement (9, 9') umfasst, wobei das Bandringelement (9, 9') mit dem rotierenden Lagerring (7, 7') mittels einer Schrumpfverbindung (22) verbunden ist, um ein Verbundelement (23) zu bilden, wobei das Verbundelement (23) mit zentrierendem Passsitz in einer Ausnehmung (8a; 32a) des Halteelements (8; 32) eingefügt ist und das Bandringelement (9, 91) mit dem Halteelement (8; 32) in Axialrichtung (X-X) der Welle (3) verbunden ist.1. Bearing arrangement for supporting a shaft (3), comprising a bearing bush (2), in which the shaft (3) is accommodated, wherein between the bearing bush (2) and the shaft (3) a circumferential annular gap (4) is present, and wherein the bearing bush (2) and the shaft (3) are made of materials having different coefficients of thermal expansion, a connection assembly (21) having a holding member (8; 32, 33, 34) connected to the shaft (3) and a rotating bearing ring (7), in order to provide a centering support of the bearing bush (2) on its outer periphery (2b) relative to the shaft (3), a stationary bearing ring (6, 6 ') which is arranged radially outside of the bearing bush (2), and with the rotating bearing ring (7, 7 1 ) forms an axial sliding bearing (14), characterized in that the connecting arrangement (21) comprises a circumferential band ring element (9, 9 '), wherein the band ring element (9, 9') with the rotating bearing ring ( 7, 7 ') by means of a Schrumpfve (22) is connected to form a composite element (23), wherein the composite element (23) with centering fit in a recess (8a; 32a) of the holding element (8; 32) is inserted and the band ring element (9, 9 1 ) with the holding element (8; 32) in the axial direction (XX) of the shaft (3) is connected.
2. Lageranordnung nach Anspruch 1 , dadurch gekennzeichnet, dass das Bandringelement (9, 9') symmetrisch zu einer Achse (A), die senkrecht zur Axialrichtung (X-X) der Welle (3) liegt, ist.2. Bearing arrangement according to claim 1, characterized in that the band ring element (9, 9 ') is symmetrical to an axis (A) which is perpendicular to the axial direction (X-X) of the shaft (3).
3. Lageranordnung nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Lagerbuchse (2), der rotierende Lagerring (7, 7') und der stationäre Lagerring (6, 6') aus einem Material mit gleichem oder ähnlichem Wärmeausdehnungskoeffizienten, insbesondere aus SiC, hergestellt sind. 3. Bearing arrangement according to claim 1 or 2, characterized in that the bearing bush (2), the rotating bearing ring (7, 7 ') and the stationary bearing ring (6, 6') made of a material having the same or similar coefficients of thermal expansion, in particular of SiC , are made.
4. Lageranordnung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das Halteelement (9; 32), die Welle (3) und das Bandringelement (9, 9') aus einem Material mit gleichem oder ähnlichem Wärmeausdehnungskoeffizienten, insbesondere aus Stahl, hergestellt sind.4. Bearing arrangement according to one of the preceding claims, characterized in that the holding element (9; 32), the shaft (3) and the band ring element (9, 9 ') are made of a material having the same or similar coefficients of thermal expansion, in particular made of steel ,
5. Lageranordnung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der stationäre Lagerring (6, 6') eine radiale Gleitfläche (6b) aufweist und mit einer radialen Gleitfläche (2b) der Lagerbuchse (2) ein Radialgleitlager (15) bildet.5. Bearing arrangement according to one of the preceding claims, characterized in that the stationary bearing ring (6, 6 ') has a radial sliding surface (6b) and with a radial sliding surface (2b) of the bearing bush (2) forms a radial sliding bearing (15).
6. Lageranordnung nach einem der vorhergehenden Ansprüche, gekennzeichnet durch zwei stationäre Lagerringe (6, 6') und zwei rotierende Lagerringe (7, 7') zur Bildung einer Doppellageranordnung.6. Bearing arrangement according to one of the preceding claims, characterized by two stationary bearing rings (6, 6 ') and two rotating bearing rings (7, 7') for forming a double bearing arrangement.
7. Lageranordnung nach Anspruch 6, dadurch gekennzeichnet, dass die rotierenden Lagerringe (7, 7') an in Axialrichtung (X-X) einander zugewandten Seiten der stationären Lagerringe (6, 6') angeordnet sind oder dass die rotierenden Lagerringe (7, 7') an in Axialrichtung (X-X) einander abgewandten Seiten der stationären Lagerringe (6, 6') angeordnet sind.7. Bearing arrangement according to claim 6, characterized in that the rotating bearing rings (7, 7 ') in the axial direction (XX) mutually facing sides of the stationary bearing rings (6, 6') are arranged or that the rotating bearing rings (7, 7 ' ) are arranged on sides of the stationary bearing rings (6, 6 ') facing away from one another in the axial direction (XX).
8. Magnetkupplung, umfassend eine Lageranordnung nach einem der vorhergehenden Ansprüche. 8. A magnetic coupling comprising a bearing assembly according to one of the preceding claims.
PCT/EP2010/001541 2009-03-25 2010-03-11 Thermally decoupled bearing arrangement WO2010108603A1 (en)

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US13/138,628 US20120068565A1 (en) 2009-03-25 2010-03-11 Thermally decoupled bearing arrangement
EP10708731A EP2411688B1 (en) 2009-03-25 2010-03-11 Thermally decoupled bearing arrangement
BRPI1014193A BRPI1014193A2 (en) 2009-03-25 2010-03-11 "thermally decoupled bearing arrangement"
JP2012500117A JP5422040B2 (en) 2009-03-25 2010-03-11 Thermally isolated bearing device
CA2753819A CA2753819C (en) 2009-03-25 2010-03-11 Thermally decoupled bearing arrangement
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EP2411688A1 (en) 2012-02-01
JP2012520431A (en) 2012-09-06
DE202009004160U1 (en) 2009-05-28
BRPI1014193A2 (en) 2016-04-26
JP5422040B2 (en) 2014-02-19
CA2753819A1 (en) 2010-09-30
MX2011009887A (en) 2011-09-30
CN102356246A (en) 2012-02-15
CA2753819C (en) 2014-12-30
CN102356246B (en) 2014-01-15
US20120068565A1 (en) 2012-03-22
EP2411688B1 (en) 2013-03-06

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